GB2196911B - Thrust reverser - Google Patents

Thrust reverser

Info

Publication number
GB2196911B
GB2196911B GB8625930A GB8625930A GB2196911B GB 2196911 B GB2196911 B GB 2196911B GB 8625930 A GB8625930 A GB 8625930A GB 8625930 A GB8625930 A GB 8625930A GB 2196911 B GB2196911 B GB 2196911B
Authority
GB
United Kingdom
Prior art keywords
thrust reverser
reverser
thrust
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
GB8625930A
Other versions
GB8625930D0 (en
GB2196911A (en
Inventor
Arnold Charles Newton
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB8625930A priority Critical patent/GB2196911B/en
Publication of GB8625930D0 publication Critical patent/GB8625930D0/en
Priority to US07/089,340 priority patent/US4823547A/en
Priority to DE19873731829 priority patent/DE3731829A1/en
Priority to JP62271593A priority patent/JPS63117152A/en
Priority to FR878714903A priority patent/FR2606080B1/en
Publication of GB2196911A publication Critical patent/GB2196911A/en
Application granted granted Critical
Publication of GB2196911B publication Critical patent/GB2196911B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
GB8625930A 1986-10-30 1986-10-30 Thrust reverser Expired - Fee Related GB2196911B (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB8625930A GB2196911B (en) 1986-10-30 1986-10-30 Thrust reverser
US07/089,340 US4823547A (en) 1986-10-30 1987-08-25 Thrust reverser
DE19873731829 DE3731829A1 (en) 1986-10-30 1987-09-22 DRAWER REVERSE FOR A GAS TURBINE ENGINE
JP62271593A JPS63117152A (en) 1986-10-30 1987-10-27 Gas turbine engine
FR878714903A FR2606080B1 (en) 1986-10-30 1987-10-28 PUSH INVERTER

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8625930A GB2196911B (en) 1986-10-30 1986-10-30 Thrust reverser

Publications (3)

Publication Number Publication Date
GB8625930D0 GB8625930D0 (en) 1987-02-04
GB2196911A GB2196911A (en) 1988-05-11
GB2196911B true GB2196911B (en) 1990-03-14

Family

ID=10606522

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8625930A Expired - Fee Related GB2196911B (en) 1986-10-30 1986-10-30 Thrust reverser

Country Status (5)

Country Link
US (1) US4823547A (en)
JP (1) JPS63117152A (en)
DE (1) DE3731829A1 (en)
FR (1) FR2606080B1 (en)
GB (1) GB2196911B (en)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5409259A (en) * 1992-10-09 1995-04-25 Morton International, Inc. Gas generator for vehicle occupant restraint system
FR2764643B1 (en) * 1997-06-12 1999-07-16 Hispano Suiza Sa PUSH INVERTER WITH TURBOREACTOR DOORS WITH VARIABLE EJECTION SECTION
US6824101B2 (en) * 2003-02-17 2004-11-30 The Boeing Company Apparatus and method for mounting a cascade support ring to a thrust reverser
GB0608985D0 (en) * 2006-05-06 2006-06-14 Rolls Royce Plc Aeroengine thrust reverser
FR2922958B1 (en) * 2007-10-25 2009-11-20 Aircelle Sa THRUST INVERTER WITH GRILLS
FR2947869B1 (en) * 2009-07-10 2011-12-09 Snecma EXTENDABLE FINS GRID FOR AN AIRCRAFT TURBOMACHINE PUSH INVERSION SYSTEM
US8869507B2 (en) * 2010-01-13 2014-10-28 United Technologies Corporation Translatable cascade thrust reverser
RU2443892C1 (en) * 2010-06-29 2012-02-27 Федеральное государственное унитарное предприятие Государственный научно-исследовательский институт гражданской авиации (ГосНИИ ГА) Method of turning gas flow in deflecting grids of gas turbine engine reversing device
DE102011008917A1 (en) 2011-01-19 2012-07-19 Rolls-Royce Deutschland Ltd & Co Kg Aircraft gas turbine thrust reverser
US9555871B2 (en) * 2012-03-05 2017-01-31 The Boeing Company Two-surface sandwich structure for accommodating in-plane expansion of one of the surfaces relative to the opposing surface
US9399951B2 (en) * 2012-04-17 2016-07-26 General Electric Company Modular louver system
US9068532B2 (en) * 2012-07-24 2015-06-30 Rohr, Inc. Translating sleeve thrust reverser with movable cascade
US10309343B2 (en) 2014-11-06 2019-06-04 Rohr, Inc. Split sleeve hidden door thrust reverser
US10018151B2 (en) * 2015-01-14 2018-07-10 The Boeing Company Methods and apparatus to vary reverse thrust of aircraft engines
US9874176B2 (en) 2015-01-14 2018-01-23 The Boeing Company Methods and apparatus to vary reverse thrust of aircraft engines
US9856018B2 (en) * 2016-01-11 2018-01-02 The Boeing Company Ducted fan doors for aircraft
US20180045140A1 (en) * 2016-08-09 2018-02-15 Rolls-Royce Plc Aircraft gas turbine engine nacelle
US11459979B2 (en) * 2021-02-02 2022-10-04 Spirit Aerosystems, Inc. Textile cascade assembly
FR3127479B1 (en) * 2021-09-24 2023-09-01 Safran Nacelles Nacelle for aircraft propulsion assembly, comprising a thrust reverser with movable grilles, and preferably at least one pivoting fan cowl

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR635013A (en) * 1927-05-25 1928-03-05 Louver refinements
US2209384A (en) * 1938-09-06 1940-07-30 Pioneer Mfg Company Exterior venetian blind
US3346007A (en) * 1962-08-22 1967-10-10 Israel State Gas flow control louvres
GB1259045A (en) * 1970-03-23 1972-01-05
US3739582A (en) * 1972-04-13 1973-06-19 Rohr Industries Inc Thrust reversing apparatus
US4030290A (en) * 1974-11-06 1977-06-21 The Boeing Company Jet engine thrust reverser
US4026105A (en) * 1975-03-25 1977-05-31 The Boeing Company Jet engine thrust reverser
US3981451A (en) * 1975-11-17 1976-09-21 Rohr Industries, Inc. Fan cascade thrust reverser
US4030291A (en) * 1976-01-02 1977-06-21 General Electric Company Thrust reverser for a gas turbofan engine
US4760960A (en) * 1987-05-22 1988-08-02 United Technologies Corporation Linkage for area controlled, thrust vectoring vane cascade

Also Published As

Publication number Publication date
FR2606080A1 (en) 1988-05-06
FR2606080B1 (en) 1992-04-10
GB8625930D0 (en) 1987-02-04
DE3731829A1 (en) 1988-05-05
GB2196911A (en) 1988-05-11
JPS63117152A (en) 1988-05-21
US4823547A (en) 1989-04-25

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20001030